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1. Identity statement
Reference TypeJournal Article
Siteplutao.sid.inpe.br
Holder Codeisadg {BR SPINPE} ibi 8JMKD3MGPCW/3DT298S
Identifier8JMKD3MGP3W/3MTN5AP
Repositorysid.inpe.br/plutao/2016/12.05.19.43.51   (restricted access)
Last Update2016:12.08.18.44.30 (UTC) administrator
Metadata Repositorysid.inpe.br/plutao/2016/12.05.19.43.52
Metadata Last Update2021:03.05.18.02.39 (UTC) administrator
ISSN0861-6663
Labellattes: 0404556644554239 1 GonçalvesRoccMoraPrad:2016:EfInTe
Citation KeyGonçalvesRoccMoraPrad:2016:EfInTe
TitleEffects of the individual terms of the lunar potential in the motion of satellites around the Moon
Year2016
Access Date2024, May 15
Type of Workjournal article
Secondary TypePRE PI
Number of Files1
Size3108 KiB
2. Context
Author1 Gonçalves, Liana Dias
2 Rocco, Evandro Marconi
3 Moraes, Rodolpho Vilhena de
4 Prado, Antonio Fernando Bertachini de Almeida
Resume Identifier1
2 8JMKD3MGP5W/3C9JH37
3
4 8JMKD3MGP5W/3C9JGJA
Group1 CMC-ETES-SPG-INPE-MCTI-GOV-BR
2 DMC-ETE-INPE-MCTI-GOV-BR
3
4 DMC-ETE-INPE-MCTI-GOV-BR
Affiliation1 Instituto Nacional de Pesquisas Espaciais (INPE)
2 Instituto Nacional de Pesquisas Espaciais (INPE)
3 Universidade Federal de São Paulo (UNIFESP)
4 Instituto Nacional de Pesquisas Espaciais (INPE)
Author e-Mail Address1 lianadgon@gmail.com
2 evandro.rocco@inpe.br
3
4 prado@dem.inpe.br
JournalInternational Journal of Theoretical and Applied Mechanics
Volume1
Pages20-29
History (UTC)2016-12-08 18:44:31 :: lattes -> administrator :: 2016
2021-03-05 18:02:39 :: administrator -> simone :: 2016
3. Content and structure
Is the master or a copy?is the master
Content Stagecompleted
Transferable1
Content TypeExternal Contribution
Version Typepublisher
KeywordsAstrodynamics
Lunar potential
Orbital Motion
Orbital Maneuvers
Satellite
Control System
AbstractThe present work study analyzes the influence of non homogeneity of the lunar gravitational field in the orbit of an artificial satellite. The model is based in spherical harmonics, according to the development presented by Konopliv. This model allows us to consider spherical harmonics until degree and order 100. Simulations are performed for the analysis of the following facts: the contribution of each term of the potential; the variation of the perturbation due to the inclination of the orbit; the actuation of the control system; the influence in transfer and correction maneuvers made to minimize the perturbative effects in the artificial satellite orbit. The transfer and correction maneuvers of lunar satellites are simulated using continuous thrust and trajectory control in closed loop.
AreaETES
Arrangement 1urlib.net > BDMCI > Fonds > Produção pgr ATUAIS > CMC > Effects of the...
Arrangement 2urlib.net > Produção anterior à 2021 > DIDMC > Effects of the...
doc Directory Contentaccess
source Directory Contentthere are no files
agreement Directory Contentthere are no files
4. Conditions of access and use
Languageen
Target Filegoncalves_effects.pdf
Reader Groupadministrator
lattes
Visibilityshown
Read Permissiondeny from all and allow from 150.163
Update Permissionnot transferred
5. Allied materials
Mirror Repositoryurlib.net/www/2011/03.29.20.55
Next Higher Units8JMKD3MGPCW/3F2UALS
8JMKD3MGPCW/446AF4B
Citing Item Listsid.inpe.br/bibdigital/2021/02.11.18.06 3
sid.inpe.br/mtc-m21/2012/07.13.14.45.41 1
sid.inpe.br/mtc-m21/2012/07.13.14.40.20 1
DisseminationPORTALCAPES; SCOPUS.
Host Collectiondpi.inpe.br/plutao@80/2008/08.19.15.01
6. Notes
Empty Fieldsalternatejournal archivingpolicy archivist callnumber copyholder copyright creatorhistory descriptionlevel doi e-mailaddress format isbn lineage mark month nextedition notes number orcid parameterlist parentrepositories previousedition previouslowerunit progress project rightsholder schedulinginformation secondarydate secondarykey secondarymark session shorttitle sponsor subject tertiarymark tertiarytype url usergroup
7. Description control
e-Mail (login)simone
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